View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 03615U 26088.10618544 +.00000000 +00000-0 +16534-4 0 00004
2 03615 101.6932 38.2170 0032184 117.6983 242.7363 12.56248464 02
| Epoch (UTC): | 29 March 2026 02:32:54 |
| Eccentricity: | 0.0032184 |
| inclination: | 101.6932° |
| perigee height: | 1413 km |
| apogee height: | 1464 km |
| right ascension of ascending node: | 38.2170° |
| argument of perigee: | 117.6983° |
| revolutions per day: | 12.56248464 |
| mean anomaly at epoch: | 242.7363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|