View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52871U 26145.40275032 +.00000000 +00000-0 +13577-3 0 00003
2 52871 53.2128 29.7432 0001112 83.6385 276.4734 15.08829650 08
| Epoch (UTC): | 25 May 2026 09:39:57 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 29.7432° |
| argument of perigee: | 83.6385° |
| revolutions per day: | 15.08829650 |
| mean anomaly at epoch: | 276.4734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|