View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37216U 26032.47742831 +.00000000 +00000-0 +13949-3 0 00000
2 37216 97.8825 218.0423 0001172 87.4014 272.7333 14.82106523 04
| Epoch (UTC): | 01 February 2026 11:27:29 |
| Eccentricity: | 0.0001172 |
| inclination: | 97.8825° |
| perigee height: | 622 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 218.0423° |
| argument of perigee: | 87.4014° |
| revolutions per day: | 14.82106523 |
| mean anomaly at epoch: | 272.7333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|