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 66499U 26145.63987632 +.00000000 +00000-0 +93267-3 0 00009
2 66499 42.9982 276.4582 0001440 276.6932 83.3756 15.27599288 06
| Epoch (UTC): | 25 May 2026 15:21:25 |
| Eccentricity: | 0.0001440 |
| inclination: | 42.9982° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 276.4582° |
| argument of perigee: | 276.6932° |
| revolutions per day: | 15.27599288 |
| mean anomaly at epoch: | 83.3756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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