View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37364U 11006A 25232.80603145 0.00000000 00000-0 00000-0 0 05
2 37364 90.1712 83.7188 0023068 253.5147 106.4813 13.11855100 04
| Epoch (UTC): | 20 August 2025 19:20:41 |
| Eccentricity: | 0.0023068 |
| inclination: | 90.1712° |
| perigee height: | 1198 km |
| apogee height: | 1233 km |
| right ascension of ascending node: | 83.7188° |
| argument of perigee: | 253.5147° |
| revolutions per day: | 13.11855100 |
| mean anomaly at epoch: | 106.4813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|