View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 01983U 26100.02557801 +.00000000 +00000-0 +21527-3 0 00001
2 01983 98.0327 18.6928 0062747 312.3338 47.2562 14.68577229 02
| Epoch (UTC): | 10 April 2026 00:36:49 |
| Eccentricity: | 0.0062747 |
| inclination: | 98.0327° |
| perigee height: | 621 km |
| apogee height: | 710 km |
| right ascension of ascending node: | 18.6928° |
| argument of perigee: | 312.3338° |
| revolutions per day: | 14.68577229 |
| mean anomaly at epoch: | 47.2562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|