View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51287U 26144.61355830 +.00000000 +00000-0 +00000-0 0 00004
2 51287 4.1139 77.5410 0003558 112.0555 247.7735 1.01221923 03
| Epoch (UTC): | 24 May 2026 14:43:31 |
| Eccentricity: | 0.0003558 |
| inclination: | 4.1139° |
| perigee height: | 35507 km |
| apogee height: | 35537 km |
| right ascension of ascending node: | 77.5410° |
| argument of perigee: | 112.0555° |
| revolutions per day: | 1.01221923 |
| mean anomaly at epoch: | 247.7735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|