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 66384U 26145.41540840 +.00000000 +00000-0 +37559-3 0 00006
2 66384 53.1587 220.4232 0001129 63.3384 296.7733 15.30190256 02
| Epoch (UTC): | 25 May 2026 09:58:11 |
| Eccentricity: | 0.0001129 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.4232° |
| argument of perigee: | 63.3384° |
| revolutions per day: | 15.30190256 |
| mean anomaly at epoch: | 296.7733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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