View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20202U 26140.20391881 +.00000000 +00000-0 +00000-0 0 00004
2 20202 12.9341 336.7074 0018037 274.4394 74.7524 0.98611557 01
| Epoch (UTC): | 20 May 2026 04:53:38 |
| Eccentricity: | 0.0018037 |
| inclination: | 12.9341° |
| perigee height: | 36182 km |
| apogee height: | 36335 km |
| right ascension of ascending node: | 336.7074° |
| argument of perigee: | 274.4394° |
| revolutions per day: | 0.98611557 |
| mean anomaly at epoch: | 74.7524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|