View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61719U 26145.30083402 +.00000000 +00000-0 +38996-4 0 00004
2 61719 53.1603 105.6615 0001305 84.2182 275.8967 15.30197956 02
| Epoch (UTC): | 25 May 2026 07:13:12 |
| Eccentricity: | 0.0001305 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.6615° |
| argument of perigee: | 84.2182° |
| revolutions per day: | 15.30197956 |
| mean anomaly at epoch: | 275.8967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|