View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67130U 26145.23555350 +.00000000 +00000-0 +64930-3 0 00001
2 67130 43.0003 96.6346 0001186 271.0833 88.9883 15.27597160 00
| Epoch (UTC): | 25 May 2026 05:39:11 |
| Eccentricity: | 0.0001186 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.6346° |
| argument of perigee: | 271.0833° |
| revolutions per day: | 15.27597160 |
| mean anomaly at epoch: | 88.9883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|