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 28908U 26103.96089530 +.00000000 +00000-0 +14150-3 0 00006
2 28908 82.4726 348.7400 0007545 319.9172 50.3353 12.55598241 08
| Epoch (UTC): | 13 April 2026 23:03:41 |
| Eccentricity: | 0.0007545 |
| inclination: | 82.4726° |
| perigee height: | 1435 km |
| apogee height: | 1447 km |
| right ascension of ascending node: | 348.7400° |
| argument of perigee: | 319.9172° |
| revolutions per day: | 12.55598241 |
| mean anomaly at epoch: | 50.3353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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