View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29252U 06029A 13144.28843551 .00003583 00000-0 24480-3 0 9020
2 29252 064.5120 068.2411 0012228 203.5143 299.8583 15.07768531377155
| Epoch (UTC): | 24 May 2013 06:55:20 |
| Eccentricity: | 0.0012228 |
| inclination: | 64.5120° |
| perigee height: | 534 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 68.2411° |
| argument of perigee: | 203.5143° |
| revolutions per day: | 15.07768531 |
| mean anomaly at epoch: | 299.8583° |
| orbit number at epoch: | 37715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|