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 28647U 26069.82474367 +.00000000 +00000-0 +49886-3 0 00002
2 28647 56.9966 241.7605 0061879 22.0724 338.2974 15.42725550 05
| Epoch (UTC): | 10 March 2026 19:47:37 |
| Eccentricity: | 0.0061879 |
| inclination: | 56.9966° |
| perigee height: | 396 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 241.7605° |
| argument of perigee: | 22.0724° |
| revolutions per day: | 15.42725550 |
| mean anomaly at epoch: | 338.2974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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