View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65260U 26135.64226064 +.00000000 +00000-0 +13465-3 0 00001
2 65260 97.5222 263.1906 0015928 77.1969 283.1552 15.15157103 04
| Epoch (UTC): | 15 May 2026 15:24:51 |
| Eccentricity: | 0.0015928 |
| inclination: | 97.5222° |
| perigee height: | 510 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 263.1906° |
| argument of perigee: | 77.1969° |
| revolutions per day: | 15.15157103 |
| mean anomaly at epoch: | 283.1552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|