View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62503U 26145.18208410 +.00000000 +00000-0 +45176-3 0 00007
2 62503 42.9985 216.6701 0001552 265.5701 94.4973 15.27588427 02
| Epoch (UTC): | 25 May 2026 04:22:12 |
| Eccentricity: | 0.0001552 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 216.6701° |
| argument of perigee: | 265.5701° |
| revolutions per day: | 15.27588427 |
| mean anomaly at epoch: | 94.4973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|