View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 04132U 26088.16215397 +.00000000 +00000-0 +61585-3 0 00009
2 04132 69.9906 92.9105 0011951 246.4250 113.5620 14.31787266 00
| Epoch (UTC): | 29 March 2026 03:53:30 |
| Eccentricity: | 0.0011951 |
| inclination: | 69.9906° |
| perigee height: | 777 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 92.9105° |
| argument of perigee: | 246.4250° |
| revolutions per day: | 14.31787266 |
| mean anomaly at epoch: | 113.5620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|