View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36095U 26070.28103543 +.00000000 +00000-0 +34402-4 0 00004
2 36095 67.1469 131.0076 0006307 244.4620 115.5813 13.97041037 03
| Epoch (UTC): | 11 March 2026 06:44:41 |
| Eccentricity: | 0.0006307 |
| inclination: | 67.1469° |
| perigee height: | 899 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 131.0076° |
| argument of perigee: | 244.4620° |
| revolutions per day: | 13.97041037 |
| mean anomaly at epoch: | 115.5813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|