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 66647U 26145.37911184 +.00000000 +00000-0 +65037-4 0 00009
2 66647 82.4997 184.7027 0010423 266.1163 93.8725 12.42898758 02
| Epoch (UTC): | 25 May 2026 09:05:55 |
| Eccentricity: | 0.0010423 |
| inclination: | 82.4997° |
| perigee height: | 1486 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 184.7027° |
| argument of perigee: | 266.1163° |
| revolutions per day: | 12.42898758 |
| mean anomaly at epoch: | 93.8725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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