View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60344U 26145.54828293 +.00000000 +00000-0 +37910-4 0 00003
2 60344 53.1605 78.5411 0001091 81.7793 278.3331 15.30190534 09
| Epoch (UTC): | 25 May 2026 13:09:31 |
| Eccentricity: | 0.0001091 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.5411° |
| argument of perigee: | 81.7793° |
| revolutions per day: | 15.30190534 |
| mean anomaly at epoch: | 278.3331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|