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 57665U 26145.36496433 +.00000000 +00000-0 +13287-4 0 00003
2 57665 53.1603 210.9169 0001100 92.7708 267.3419 15.30188229 03
| Epoch (UTC): | 25 May 2026 08:45:32 |
| Eccentricity: | 0.0001100 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.9169° |
| argument of perigee: | 92.7708° |
| revolutions per day: | 15.30188229 |
| mean anomaly at epoch: | 267.3419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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