View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51839U 26145.61845595 +.00000000 +00000-0 +10387-2 0 00001
2 51839 97.3646 242.3054 0007542 234.4519 125.6057 16.00588552 05
| Epoch (UTC): | 25 May 2026 14:50:34 |
| Eccentricity: | 0.0007542 |
| inclination: | 97.3646° |
| perigee height: | 268 km |
| apogee height: | 278 km |
| right ascension of ascending node: | 242.3054° |
| argument of perigee: | 234.4519° |
| revolutions per day: | 16.00588552 |
| mean anomaly at epoch: | 125.6057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|