View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00107U 26049.04411703 +.00000000 +00000-0 +58334-3 0 00008
2 00107 28.7753 283.1768 0495554 95.8199 269.9064 14.21546112 03
| Epoch (UTC): | 18 February 2026 01:03:31 |
| Eccentricity: | 0.0495554 |
| inclination: | 28.7753° |
| perigee height: | 463 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 283.1768° |
| argument of perigee: | 95.8199° |
| revolutions per day: | 14.21546112 |
| mean anomaly at epoch: | 269.9064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|