View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24971U 26041.89933176 +.00000000 +00000-0 +90440-4 0 00006
2 24971 98.8361 33.1877 0051135 239.1721 120.4427 14.35455865 05
| Epoch (UTC): | 10 February 2026 21:35:02 |
| Eccentricity: | 0.0051135 |
| inclination: | 98.8361° |
| perigee height: | 737 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 33.1877° |
| argument of perigee: | 239.1721° |
| revolutions per day: | 14.35455865 |
| mean anomaly at epoch: | 120.4427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|