View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 53711U 26145.30934448 +.00000000 +00000-0 +57975-4 0 00000
2 53711 53.2136 264.9638 0000978 113.4254 246.6841 15.08837645 09
| Epoch (UTC): | 25 May 2026 07:25:27 |
| Eccentricity: | 0.0000978 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 264.9638° |
| argument of perigee: | 113.4254° |
| revolutions per day: | 15.08837645 |
| mean anomaly at epoch: | 246.6841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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