View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27869U 26145.61501402 +.00000000 +00000-0 -19492-3 0 00001
2 27869 82.4710 340.3975 0023166 99.5626 260.8074 12.45502642 00
| Epoch (UTC): | 25 May 2026 14:45:37 |
| Eccentricity: | 0.0023166 |
| inclination: | 82.4710° |
| perigee height: | 1465 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 340.3975° |
| argument of perigee: | 99.5626° |
| revolutions per day: | 12.45502642 |
| mean anomaly at epoch: | 260.8074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|