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 66097U 26145.28346612 +.00000000 +00000-0 +43988-3 0 00006
2 66097 53.1604 107.9436 0001375 80.1190 279.9966 15.30204643 00
| Epoch (UTC): | 25 May 2026 06:48:11 |
| Eccentricity: | 0.0001375 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 107.9436° |
| argument of perigee: | 80.1190° |
| revolutions per day: | 15.30204643 |
| mean anomaly at epoch: | 279.9966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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