View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57761U 26145.38635543 +.00000000 +00000-0 +85592-4 0 00007
2 57761 81.0007 29.8286 0006403 92.2569 267.9320 13.85098030 01
| Epoch (UTC): | 25 May 2026 09:16:21 |
| Eccentricity: | 0.0006403 |
| inclination: | 81.0007° |
| perigee height: | 941 km |
| apogee height: | 951 km |
| right ascension of ascending node: | 29.8286° |
| argument of perigee: | 92.2569° |
| revolutions per day: | 13.85098030 |
| mean anomaly at epoch: | 267.9320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|