View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28493U 26159.65131295 +.00000000 +00000-0 +15682-3 0 00009
2 28493 98.2266 296.1042 0003283 338.1159 21.9911 14.80143516 07
| Epoch (UTC): | 08 June 2026 15:37:53 |
| Eccentricity: | 0.0003283 |
| inclination: | 98.2266° |
| perigee height: | 627 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 296.1042° |
| argument of perigee: | 338.1159° |
| revolutions per day: | 14.80143516 |
| mean anomaly at epoch: | 21.9911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|