View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68103U 26145.58536647 +.00000000 +00000-0 +80538-3 0 00000
2 68103 97.2839 106.1485 0001847 92.4989 267.6465 15.33443565 09
| Epoch (UTC): | 25 May 2026 14:02:55 |
| Eccentricity: | 0.0001847 |
| inclination: | 97.2839° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 106.1485° |
| argument of perigee: | 92.4989° |
| revolutions per day: | 15.33443565 |
| mean anomaly at epoch: | 267.6465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|