View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62751U 26145.51386345 +.00000000 +00000-0 +46759-3 0 00001
2 62751 42.9980 84.2478 0000670 252.5216 107.5562 15.27585334 03
| Epoch (UTC): | 25 May 2026 12:19:57 |
| Eccentricity: | 0.0000670 |
| inclination: | 42.9980° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 84.2478° |
| argument of perigee: | 252.5216° |
| revolutions per day: | 15.27585334 |
| mean anomaly at epoch: | 107.5562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|