View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27718U 26145.21016752 +.00000000 +00000-0 +00000-0 0 00000
2 27718 4.6466 76.0274 0002914 355.8291 34.1297 1.00269898 07
| Epoch (UTC): | 25 May 2026 05:02:38 |
| Eccentricity: | 0.0002914 |
| inclination: | 4.6466° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 76.0274° |
| argument of perigee: | 355.8291° |
| revolutions per day: | 1.00269898 |
| mean anomaly at epoch: | 34.1297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|