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 55663U 26145.52189976 +.00000000 +00000-0 +56300-4 0 00001
2 55663 69.9993 330.7180 0002769 264.4040 95.6804 14.98319956 05
| Epoch (UTC): | 25 May 2026 12:31:32 |
| Eccentricity: | 0.0002769 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.7180° |
| argument of perigee: | 264.4040° |
| revolutions per day: | 14.98319956 |
| mean anomaly at epoch: | 95.6804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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