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 57115U 26145.43009674 +.00000000 +00000-0 +13485-2 0 00006
2 57115 42.9979 198.4536 0020628 333.8296 26.1507 15.16090833 06
| Epoch (UTC): | 25 May 2026 10:19:20 |
| Eccentricity: | 0.0020628 |
| inclination: | 42.9979° |
| perigee height: | 503 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 198.4536° |
| argument of perigee: | 333.8296° |
| revolutions per day: | 15.16090833 |
| mean anomaly at epoch: | 26.1507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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