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 66693U 26145.14294186 +.00000000 +00000-0 +42181-3 0 00005
2 66693 97.4178 219.3388 0005651 100.4801 259.7072 15.21994590 00
| Epoch (UTC): | 25 May 2026 03:25:50 |
| Eccentricity: | 0.0005651 |
| inclination: | 97.4178° |
| perigee height: | 496 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 219.3388° |
| argument of perigee: | 100.4801° |
| revolutions per day: | 15.21994590 |
| mean anomaly at epoch: | 259.7072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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