View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 69099U 26135.82925338 +.00000000 +00000-0 +34035-4 0 00002
2 69099 97.5086 218.5071 0012918 274.2037 85.7716 15.10839506 02
| Epoch (UTC): | 15 May 2026 19:54:07 |
| Eccentricity: | 0.0012918 |
| inclination: | 97.5086° |
| perigee height: | 525 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 218.5071° |
| argument of perigee: | 274.2037° |
| revolutions per day: | 15.10839506 |
| mean anomaly at epoch: | 85.7716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|