View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26063U 26106.73697093 +.00000000 +00000-0 +36957-4 0 00003
2 26063 100.1893 32.2367 0035384 207.8142 152.1148 14.37942327 05
| Epoch (UTC): | 16 April 2026 17:41:14 |
| Eccentricity: | 0.0035384 |
| inclination: | 100.1893° |
| perigee height: | 740 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 32.2367° |
| argument of perigee: | 207.8142° |
| revolutions per day: | 14.37942327 |
| mean anomaly at epoch: | 152.1148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|