View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24277U 96046A 24358.12583592 .00000318 00000-0 14079-3 0 9990
2 24277 98.8774 32.9798 0000504 201.1025 159.0136 14.30131128478542
| Epoch (UTC): | 23 December 2024 03:01:12 |
| Eccentricity: | 0.0000504 |
| inclination: | 98.8774° |
| perigee height: | 791 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 32.9798° |
| argument of perigee: | 201.1025° |
| revolutions per day: | 14.30131128 |
| mean anomaly at epoch: | 159.0136° |
| orbit number at epoch: | 47854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|