View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28650U 26040.61808407 +.00000000 +00000-0 +32968-3 0 00001
2 28650 98.0016 58.3292 0021474 107.6448 252.7127 15.08415445 07
| Epoch (UTC): | 09 February 2026 14:50:02 |
| Eccentricity: | 0.0021474 |
| inclination: | 98.0016° |
| perigee height: | 526 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 58.3292° |
| argument of perigee: | 107.6448° |
| revolutions per day: | 15.08415445 |
| mean anomaly at epoch: | 252.7127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|