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 59247U 26145.50204543 +.00000000 +00000-0 +36801-4 0 00003
2 59247 43.0045 66.2652 0000969 274.2615 85.8126 15.27577406 07
| Epoch (UTC): | 25 May 2026 12:02:56 |
| Eccentricity: | 0.0000969 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.2652° |
| argument of perigee: | 274.2615° |
| revolutions per day: | 15.27577406 |
| mean anomaly at epoch: | 85.8126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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