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 53673U 26145.61340782 +.00000000 +00000-0 +24510-3 0 00001
2 53673 97.6045 27.5081 0002251 84.0420 276.1068 15.14716782 00
| Epoch (UTC): | 25 May 2026 14:43:18 |
| Eccentricity: | 0.0002251 |
| inclination: | 97.6045° |
| perigee height: | 520 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 27.5081° |
| argument of perigee: | 84.0420° |
| revolutions per day: | 15.14716782 |
| mean anomaly at epoch: | 276.1068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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