View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26997U 26150.37937880 +.00000000 +00000-0 +40177-4 0 00008
2 26997 66.0383 110.8960 0008724 279.8192 247.2178 12.84087218 07
| Epoch (UTC): | 30 May 2026 09:06:18 |
| Eccentricity: | 0.0008724 |
| inclination: | 66.0383° |
| perigee height: | 1318 km |
| apogee height: | 1332 km |
| right ascension of ascending node: | 110.8960° |
| argument of perigee: | 279.8192° |
| revolutions per day: | 12.84087218 |
| mean anomaly at epoch: | 247.2178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|