View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65370U 26145.35477762 +.00000000 +00000-0 +62155-3 0 00005
2 65370 53.1582 172.0301 0001036 84.2844 275.8275 15.30198901 04
| Epoch (UTC): | 25 May 2026 08:30:52 |
| Eccentricity: | 0.0001036 |
| inclination: | 53.1582° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 172.0301° |
| argument of perigee: | 84.2844° |
| revolutions per day: | 15.30198901 |
| mean anomaly at epoch: | 275.8275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|