View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62993U 26145.38631683 +.00000000 +00000-0 +20768-2 0 00003
2 62993 43.0000 259.2558 0002369 246.8045 113.2574 15.70995446 06
| Epoch (UTC): | 25 May 2026 09:16:17 |
| Eccentricity: | 0.0002369 |
| inclination: | 43.0000° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 259.2558° |
| argument of perigee: | 246.8045° |
| revolutions per day: | 15.70995446 |
| mean anomaly at epoch: | 113.2574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|