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 66248U 26145.65159836 +.00000000 +00000-0 +74040-3 0 00008
2 66248 53.1623 286.1348 0000435 99.5304 260.5747 15.31699856 06
| Epoch (UTC): | 25 May 2026 15:38:18 |
| Eccentricity: | 0.0000435 |
| inclination: | 53.1623° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 286.1348° |
| argument of perigee: | 99.5304° |
| revolutions per day: | 15.31699856 |
| mean anomaly at epoch: | 260.5747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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