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 66348U 26145.51146024 +.00000000 +00000-0 +21842-3 0 00001
2 66348 53.1596 235.8942 0001391 91.3511 268.7649 15.30197507 05
| Epoch (UTC): | 25 May 2026 12:16:30 |
| Eccentricity: | 0.0001391 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.8942° |
| argument of perigee: | 91.3511° |
| revolutions per day: | 15.30197507 |
| mean anomaly at epoch: | 268.7649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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