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 66819U 26145.42313367 +.00000000 +00000-0 +51283-3 0 00002
2 66819 43.0039 41.0794 0001490 269.9661 90.1020 15.27596209 07
| Epoch (UTC): | 25 May 2026 10:09:18 |
| Eccentricity: | 0.0001490 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.0794° |
| argument of perigee: | 269.9661° |
| revolutions per day: | 15.27596209 |
| mean anomaly at epoch: | 90.1020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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