View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 09803U 26150.59560932 +.00000000 +00000-0 +00000-0 0 00006
2 09803 4.7695 284.5172 0078624 39.1295 0.6838 0.97529242 03
| Epoch (UTC): | 30 May 2026 14:17:40 |
| Eccentricity: | 0.0078624 |
| inclination: | 4.7695° |
| perigee height: | 36236 km |
| apogee height: | 36911 km |
| right ascension of ascending node: | 284.5172° |
| argument of perigee: | 39.1295° |
| revolutions per day: | 0.97529242 |
| mean anomaly at epoch: | 0.6838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|