View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28737U 26145.46484784 +.00000000 +00000-0 +33379-3 0 00001
2 28737 97.7304 174.9628 0017582 110.0691 250.2438 15.21136111 03
| Epoch (UTC): | 25 May 2026 11:09:22 |
| Eccentricity: | 0.0017582 |
| inclination: | 97.7304° |
| perigee height: | 490 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 174.9628° |
| argument of perigee: | 110.0691° |
| revolutions per day: | 15.21136111 |
| mean anomaly at epoch: | 250.2438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|