View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00202U 26039.10084626 +.00000000 +00000-0 +58780-4 0 00006
2 00202 32.4381 288.8764 0101226 314.0022 45.2291 13.63779981 01
| Epoch (UTC): | 08 February 2026 02:25:13 |
| Eccentricity: | 0.0101226 |
| inclination: | 32.4381° |
| perigee height: | 947 km |
| apogee height: | 1097 km |
| right ascension of ascending node: | 288.8764° |
| argument of perigee: | 314.0022° |
| revolutions per day: | 13.63779981 |
| mean anomaly at epoch: | 45.2291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|