View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63600U 26145.57806652 +.00000000 +00000-0 +94263-4 0 00003
2 63600 99.6913 153.1179 0001159 80.2624 279.8645 13.57244090 05
| Epoch (UTC): | 25 May 2026 13:52:24 |
| Eccentricity: | 0.0001159 |
| inclination: | 99.6913° |
| perigee height: | 1045 km |
| apogee height: | 1047 km |
| right ascension of ascending node: | 153.1179° |
| argument of perigee: | 80.2624° |
| revolutions per day: | 13.57244090 |
| mean anomaly at epoch: | 279.8645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|