View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62249U 26145.60678521 +.00000000 +00000-0 +13110-3 0 00008
2 62249 89.0101 24.7554 0019126 86.3298 274.0040 13.51009000 02
| Epoch (UTC): | 25 May 2026 14:33:46 |
| Eccentricity: | 0.0019126 |
| inclination: | 89.0101° |
| perigee height: | 1054 km |
| apogee height: | 1083 km |
| right ascension of ascending node: | 24.7554° |
| argument of perigee: | 86.3298° |
| revolutions per day: | 13.51009000 |
| mean anomaly at epoch: | 274.0040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|