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 65615U 26145.15256101 +.00000000 +00000-0 -32365-4 0 00009
2 65615 97.4502 213.6137 0002224 162.3330 197.7975 15.05642489 02
| Epoch (UTC): | 25 May 2026 03:39:41 |
| Eccentricity: | 0.0002224 |
| inclination: | 97.4502° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.6137° |
| argument of perigee: | 162.3330° |
| revolutions per day: | 15.05642489 |
| mean anomaly at epoch: | 197.7975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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