View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60731U 26145.24828580 +.00000000 +00000-0 +11346-4 0 00004
2 60731 53.1602 98.5419 0001188 102.4968 257.6183 15.69711143 00
| Epoch (UTC): | 25 May 2026 05:57:31 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.1602° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 98.5419° |
| argument of perigee: | 102.4968° |
| revolutions per day: | 15.69711143 |
| mean anomaly at epoch: | 257.6183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|