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 66460U 26145.55556536 +.00000000 +00000-0 +93352-3 0 00008
2 66460 42.9993 221.9374 0001647 263.7676 96.2988 15.27602410 03
| Epoch (UTC): | 25 May 2026 13:20:00 |
| Eccentricity: | 0.0001647 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 221.9374° |
| argument of perigee: | 263.7676° |
| revolutions per day: | 15.27602410 |
| mean anomaly at epoch: | 96.2988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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