View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49092U 26145.38748458 +.00000000 +00000-0 +70751-4 0 00006
2 49092 87.9153 10.4045 0001865 89.0610 271.0735 13.17650987 09
| Epoch (UTC): | 25 May 2026 09:17:58 |
| Eccentricity: | 0.0001865 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4045° |
| argument of perigee: | 89.0610° |
| revolutions per day: | 13.17650987 |
| mean anomaly at epoch: | 271.0735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|