View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67274U 26145.61996700 +.00000000 +00000-0 +30162-3 0 00000
2 67274 97.3937 220.5584 0016339 85.5130 274.7973 15.22193712 08
| Epoch (UTC): | 25 May 2026 14:52:45 |
| Eccentricity: | 0.0016339 |
| inclination: | 97.3937° |
| perigee height: | 488 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 220.5584° |
| argument of perigee: | 85.5130° |
| revolutions per day: | 15.22193712 |
| mean anomaly at epoch: | 274.7973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|