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 65293U 26145.40748321 +.00000000 +00000-0 +11294-3 0 00005
2 65293 97.4517 197.8943 0001495 120.0574 240.0801 15.05656307 02
| Epoch (UTC): | 25 May 2026 09:46:46 |
| Eccentricity: | 0.0001495 |
| inclination: | 97.4517° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 197.8943° |
| argument of perigee: | 120.0574° |
| revolutions per day: | 15.05656307 |
| mean anomaly at epoch: | 240.0801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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