View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24279U 26160.72115046 +.00000000 +00000-0 +64136-4 0 00002
2 24279 98.7587 99.6598 0298815 203.0438 219.5333 13.47482095 08
| Epoch (UTC): | 09 June 2026 17:18:27 |
| Eccentricity: | 0.0298815 |
| inclination: | 98.7587° |
| perigee height: | 859 km |
| apogee height: | 1304 km |
| right ascension of ascending node: | 99.6598° |
| argument of perigee: | 203.0438° |
| revolutions per day: | 13.47482095 |
| mean anomaly at epoch: | 219.5333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|