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 53063U 26145.38868176 +.00000000 +00000-0 -46142-4 0 00007
2 53063 97.4467 326.3777 0001094 131.9080 228.2241 15.05665082 06
| Epoch (UTC): | 25 May 2026 09:19:42 |
| Eccentricity: | 0.0001094 |
| inclination: | 97.4467° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 326.3777° |
| argument of perigee: | 131.9080° |
| revolutions per day: | 15.05665082 |
| mean anomaly at epoch: | 228.2241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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