View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65953U 26145.34710109 +.00000000 +00000-0 +47563-3 0 00002
2 65953 51.8996 16.5889 0000708 106.8574 253.2466 14.79932978 08
| Epoch (UTC): | 25 May 2026 08:19:49 |
| Eccentricity: | 0.0000708 |
| inclination: | 51.8996° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 16.5889° |
| argument of perigee: | 106.8574° |
| revolutions per day: | 14.79932978 |
| mean anomaly at epoch: | 253.2466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|