View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23087U 26158.91150778 +.00000000 +00000-0 +22703-3 0 00000
2 23087 71.0541 346.3332 0010603 253.7139 106.2817 14.14392657 01
| Epoch (UTC): | 07 June 2026 21:52:34 |
| Eccentricity: | 0.0010603 |
| inclination: | 71.0541° |
| perigee height: | 837 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 346.3332° |
| argument of perigee: | 253.7139° |
| revolutions per day: | 14.14392657 |
| mean anomaly at epoch: | 106.2817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|