View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29110U 26111.52699008 +.00000000 +00000-0 +11594-2 0 00008
2 29110 98.3271 31.2953 0005218 134.3069 225.8596 15.26607521 02
| Epoch (UTC): | 21 April 2026 12:38:51 |
| Eccentricity: | 0.0005218 |
| inclination: | 98.3271° |
| perigee height: | 482 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 31.2953° |
| argument of perigee: | 134.3069° |
| revolutions per day: | 15.26607521 |
| mean anomaly at epoch: | 225.8596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|