View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39474U 26145.55447441 +.00000000 +00000-0 +99377-3 0 00000
2 39474 120.4512 44.4297 0070022 28.5965 331.8943 15.59362083 03
| Epoch (UTC): | 25 May 2026 13:18:26 |
| Eccentricity: | 0.0070022 |
| inclination: | 120.4512° |
| perigee height: | 342 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 44.4297° |
| argument of perigee: | 28.5965° |
| revolutions per day: | 15.59362083 |
| mean anomaly at epoch: | 331.8943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|