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 55676U 26145.44256030 +.00000000 +00000-0 +31936-3 0 00009
2 55676 70.0006 310.9697 0002648 267.6318 92.4538 14.98341788 06
| Epoch (UTC): | 25 May 2026 10:37:17 |
| Eccentricity: | 0.0002648 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.9697° |
| argument of perigee: | 267.6318° |
| revolutions per day: | 14.98341788 |
| mean anomaly at epoch: | 92.4538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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