View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62908U 26145.55277279 +.00000000 +00000-0 +14940-2 0 00000
2 62908 43.0007 244.0943 0000821 182.0437 178.0428 15.70866274 09
| Epoch (UTC): | 25 May 2026 13:15:59 |
| Eccentricity: | 0.0000821 |
| inclination: | 43.0007° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 244.0943° |
| argument of perigee: | 182.0437° |
| revolutions per day: | 15.70866274 |
| mean anomaly at epoch: | 178.0428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|