View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60301U 26145.36344619 +.00000000 +00000-0 +13454-4 0 00008
2 60301 53.1595 128.4661 0001057 85.9951 274.1187 15.69709121 09
| Epoch (UTC): | 25 May 2026 08:43:21 |
| Eccentricity: | 0.0001057 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 128.4661° |
| argument of perigee: | 85.9951° |
| revolutions per day: | 15.69709121 |
| mean anomaly at epoch: | 274.1187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|