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 65453U 26145.10269400 +.00000000 +00000-0 +19182-3 0 00000
2 65453 97.5140 0.2491 0001749 80.5294 279.6130 15.04837683 09
| Epoch (UTC): | 25 May 2026 02:27:52 |
| Eccentricity: | 0.0001749 |
| inclination: | 97.5140° |
| perigee height: | 551 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 0.2491° |
| argument of perigee: | 80.5294° |
| revolutions per day: | 15.04837683 |
| mean anomaly at epoch: | 279.6130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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