Column
|
Description
|
Line 1
|
Line number of element data
|
Lines 03 - 07
|
Satellite number
|
Lines 09 - 16
|
Inclination (degrees)
|
Lines 18 - 25
|
Right ascension of the ascending node
(degrees)
|
Lines 27 - 33
|
Eccentricity (decimal point assumed)
|
Lines 35 - 42
|
Argument of perigee (degrees)
|
Lines 44 - 51
|
Mean anomaly (degrees)
|
Lines 53 - 63
|
Mean motion (revolutions per day)
|
Lines 64 - 68
|
Revolution number at epoch (revolutions)
|
Line 69
|
Checksum (modulo 10)
|
Column | Description |
Line 1 | Line number of element data |
Lines 03 - 07 | Satellite number |
Lines 08 | Classification (U=unclassified) |
Lines 10 - 11 |
International Designator (last two digits of launch year) |
Lines 12 - 14 |
International Designator (launch number of the year) |
Lines 15 - 17 | International Designator (piece of the launch) |
Lines 19 - 20 | Epoch Year (las two digits of year) |
Lines 21 - 32 |
Epoch (day of the year & fractional portion of day) |
Lines 34 - 43 | First time derivative of the mean motion |
Lines 45 - 52 |
Second time derivative of mean motion (decimal point assumed) |
Lines 54 - 61 |
BSTAR drag term (decimal point assumed) |
Line 63 | Ephemeris type |
Lines 65 - 68 | Element number |
Line 69 |
Checksum (Modulo 10) (Letter, blanks, periods, plus signs = 0; minus signs = 1) |