View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28369U 26145.46733360 +.00000000 +00000-0 +90162-4 0 00003
2 28369 98.5775 154.9861 0033436 93.1136 267.3887 14.55452096 09
| Epoch (UTC): | 25 May 2026 11:12:57 |
| Eccentricity: | 0.0033436 |
| inclination: | 98.5775° |
| perigee height: | 684 km |
| apogee height: | 732 km |
| right ascension of ascending node: | 154.9861° |
| argument of perigee: | 93.1136° |
| revolutions per day: | 14.55452096 |
| mean anomaly at epoch: | 267.3887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|