View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13028U 26075.86593706 +.00000000 +00000-0 +11095-3 0 00000
2 13028 74.0381 259.8565 0020183 272.2787 87.6057 14.39880921 06
| Epoch (UTC): | 16 March 2026 20:46:56 |
| Eccentricity: | 0.0020183 |
| inclination: | 74.0381° |
| perigee height: | 744 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 259.8565° |
| argument of perigee: | 272.2787° |
| revolutions per day: | 14.39880921 |
| mean anomaly at epoch: | 87.6057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|