View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61640U 26145.53861786 +.00000000 +00000-0 +49098-4 0 00006
2 61640 43.0028 80.1363 0000831 258.3661 101.7097 15.27575518 01
| Epoch (UTC): | 25 May 2026 12:55:36 |
| Eccentricity: | 0.0000831 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.1363° |
| argument of perigee: | 258.3661° |
| revolutions per day: | 15.27575518 |
| mean anomaly at epoch: | 101.7097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|