View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66972U 26145.15493581 +.00000000 +00000-0 +51222-3 0 00002
2 66972 42.9993 311.4587 0000404 297.9034 62.1777 15.27589081 05
| Epoch (UTC): | 25 May 2026 03:43:06 |
| Eccentricity: | 0.0000404 |
| inclination: | 42.9993° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 311.4587° |
| argument of perigee: | 297.9034° |
| revolutions per day: | 15.27589081 |
| mean anomaly at epoch: | 62.1777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|