View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62811U 26145.18397644 +.00000000 +00000-0 +57473-3 0 00000
2 62811 53.1607 314.0266 0001780 90.8003 269.3202 15.30202773 04
| Epoch (UTC): | 25 May 2026 04:24:55 |
| Eccentricity: | 0.0001780 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.0266° |
| argument of perigee: | 90.8003° |
| revolutions per day: | 15.30202773 |
| mean anomaly at epoch: | 269.3202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|