View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49296U 26145.36963029 +.00000000 +00000-0 +13284-3 0 00000
2 49296 87.9176 278.9893 0001806 108.1016 252.0314 13.20773661 01
| Epoch (UTC): | 25 May 2026 08:52:16 |
| Eccentricity: | 0.0001806 |
| inclination: | 87.9176° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9893° |
| argument of perigee: | 108.1016° |
| revolutions per day: | 13.20773661 |
| mean anomaly at epoch: | 252.0314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|