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 66079U 26145.56356227 +.00000000 +00000-0 +23928-3 0 00002
2 66079 53.1586 248.0207 0001001 96.1801 263.9314 15.30197908 09
| Epoch (UTC): | 25 May 2026 13:31:31 |
| Eccentricity: | 0.0001001 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.0207° |
| argument of perigee: | 96.1801° |
| revolutions per day: | 15.30197908 |
| mean anomaly at epoch: | 263.9314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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