View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57370U 26145.55857711 +.00000000 +00000-0 +37182-4 0 00007
2 57370 43.0023 167.7038 0000644 274.2701 85.8078 15.27579327 09
| Epoch (UTC): | 25 May 2026 13:24:21 |
| Eccentricity: | 0.0000644 |
| inclination: | 43.0023° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 167.7038° |
| argument of perigee: | 274.2701° |
| revolutions per day: | 15.27579327 |
| mean anomaly at epoch: | 85.8078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|