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 53466U 26145.66668980 +.00000000 +00000-0 +36056-2 0 00006
2 53466 97.6023 267.6428 0001258 93.3226 200.6564 15.41435780 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001258 |
| inclination: | 97.6023° |
| perigee height: | 441 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 267.6428° |
| argument of perigee: | 93.3226° |
| revolutions per day: | 15.41435780 |
| mean anomaly at epoch: | 200.6564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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