View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60499U 26145.58602191 +.00000000 +00000-0 +18662-2 0 00006
2 60499 97.3786 230.4434 0001515 181.9061 178.2186 15.50653350 04
| Epoch (UTC): | 25 May 2026 14:03:52 |
| Eccentricity: | 0.0001515 |
| inclination: | 97.3786° |
| perigee height: | 414 km |
| apogee height: | 416 km |
| right ascension of ascending node: | 230.4434° |
| argument of perigee: | 181.9061° |
| revolutions per day: | 15.50653350 |
| mean anomaly at epoch: | 178.2186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|