View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49095U 26145.61193502 +.00000000 +00000-0 -29057-5 0 00004
2 49095 87.9151 10.3529 0001403 96.8408 263.2883 13.17649722 07
| Epoch (UTC): | 25 May 2026 14:41:11 |
| Eccentricity: | 0.0001403 |
| inclination: | 87.9151° |
| perigee height: | 1193 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3529° |
| argument of perigee: | 96.8408° |
| revolutions per day: | 13.17649722 |
| mean anomaly at epoch: | 263.2883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|