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 65702U 26145.55275497 +.00000000 +00000-0 +10095-2 0 00002
2 65702 53.1614 348.5051 0001884 79.9762 280.1451 15.30224638 04
| Epoch (UTC): | 25 May 2026 13:15:58 |
| Eccentricity: | 0.0001884 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 348.5051° |
| argument of perigee: | 79.9762° |
| revolutions per day: | 15.30224638 |
| mean anomaly at epoch: | 280.1451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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