View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65180U 26145.61655243 +.00000000 +00000-0 +24226-3 0 00002
2 65180 97.4474 18.0635 0002065 74.9156 285.2300 15.05658742 08
| Epoch (UTC): | 25 May 2026 14:47:50 |
| Eccentricity: | 0.0002065 |
| inclination: | 97.4474° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 18.0635° |
| argument of perigee: | 74.9156° |
| revolutions per day: | 15.05658742 |
| mean anomaly at epoch: | 285.2300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|