View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24971U 26105.88700315 +.00000000 +00000-0 +45878-4 0 00008
2 24971 98.8422 98.7403 0053028 52.1693 308.4274 14.35490217 07
| Epoch (UTC): | 15 April 2026 21:17:17 |
| Eccentricity: | 0.0053028 |
| inclination: | 98.8422° |
| perigee height: | 736 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 98.7403° |
| argument of perigee: | 52.1693° |
| revolutions per day: | 14.35490217 |
| mean anomaly at epoch: | 308.4274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|