View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00877U 26087.92180757 +.00000000 +00000-0 +64749-4 0 00001
2 00877 65.0756 274.8505 0080415 286.1773 73.0488 14.61381015 06
| Epoch (UTC): | 28 March 2026 22:07:24 |
| Eccentricity: | 0.0080415 |
| inclination: | 65.0756° |
| perigee height: | 632 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 274.8505° |
| argument of perigee: | 286.1773° |
| revolutions per day: | 14.61381015 |
| mean anomaly at epoch: | 73.0488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|