View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63077U 26145.42202875 +.00000000 +00000-0 +23696-3 0 00003
2 63077 70.0004 161.0756 0004116 265.2405 94.8284 14.98343647 02
| Epoch (UTC): | 25 May 2026 10:07:43 |
| Eccentricity: | 0.0004116 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 161.0756° |
| argument of perigee: | 265.2405° |
| revolutions per day: | 14.98343647 |
| mean anomaly at epoch: | 94.8284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|