View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65485U 26144.68657767 +.00000000 +00000-0 +10937-2 0 00002
2 65485 53.1582 264.8395 0001190 80.6945 279.4190 15.30192621 06
| Epoch (UTC): | 24 May 2026 16:28:40 |
| Eccentricity: | 0.0001190 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 264.8395° |
| argument of perigee: | 80.6945° |
| revolutions per day: | 15.30192621 |
| mean anomaly at epoch: | 279.4190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|