View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62453U 26145.51695441 +.00000000 +00000-0 +79811-3 0 00005
2 62453 53.1601 338.2605 0001575 87.2373 272.8808 15.30206850 08
| Epoch (UTC): | 25 May 2026 12:24:24 |
| Eccentricity: | 0.0001575 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.2605° |
| argument of perigee: | 87.2373° |
| revolutions per day: | 15.30206850 |
| mean anomaly at epoch: | 272.8808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|