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 65516U 26144.69352860 +.00000000 +00000-0 -18403-3 0 00002
2 65516 53.1601 278.1717 0001005 80.3352 279.7762 15.30206664 04
| Epoch (UTC): | 24 May 2026 16:38:40 |
| Eccentricity: | 0.0001005 |
| inclination: | 53.1601° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 278.1717° |
| argument of perigee: | 80.3352° |
| revolutions per day: | 15.30206664 |
| mean anomaly at epoch: | 279.7762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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