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 65282U 26145.57363793 +.00000000 +00000-0 +17484-3 0 00004
2 65282 97.4501 198.1311 0001078 140.1773 219.9534 15.05654446 07
| Epoch (UTC): | 25 May 2026 13:46:02 |
| Eccentricity: | 0.0001078 |
| inclination: | 97.4501° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 198.1311° |
| argument of perigee: | 140.1773° |
| revolutions per day: | 15.05654446 |
| mean anomaly at epoch: | 219.9534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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