View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60147U 26145.52738005 +.00000000 +00000-0 +43799-4 0 00005
2 60147 53.1615 322.7891 0000993 97.9394 262.1719 15.30191313 00
| Epoch (UTC): | 25 May 2026 12:39:25 |
| Eccentricity: | 0.0000993 |
| inclination: | 53.1615° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 322.7891° |
| argument of perigee: | 97.9394° |
| revolutions per day: | 15.30191313 |
| mean anomaly at epoch: | 262.1719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|