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 59965U 26145.40864571 +.00000000 +00000-0 +17798-3 0 00005
2 59965 97.5292 300.1399 0010256 326.6783 33.3807 15.23393377 01
| Epoch (UTC): | 25 May 2026 09:48:26 |
| Eccentricity: | 0.0010256 |
| inclination: | 97.5292° |
| perigee height: | 489 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 300.1399° |
| argument of perigee: | 326.6783° |
| revolutions per day: | 15.23393377 |
| mean anomaly at epoch: | 33.3807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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