View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67315U 26145.59808245 +.00000000 +00000-0 +51631-3 0 00003
2 67315 42.9995 250.7053 0001204 277.9254 82.1461 15.27593079 07
| Epoch (UTC): | 25 May 2026 14:21:14 |
| Eccentricity: | 0.0001204 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.7053° |
| argument of perigee: | 277.9254° |
| revolutions per day: | 15.27593079 |
| mean anomaly at epoch: | 82.1461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|