View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66948U 26145.58335647 +.00000000 +00000-0 +12354-2 0 00002
2 66948 53.1602 1.2424 0001204 97.3869 134.9114 15.34370831 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 1.2424° |
| argument of perigee: | 97.3869° |
| revolutions per day: | 15.34370831 |
| mean anomaly at epoch: | 134.9114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|