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 57986U 26145.18763712 +.00000000 +00000-0 +36713-3 0 00004
2 57986 35.0009 57.1691 0005262 309.7163 50.3087 15.23059580 08
| Epoch (UTC): | 25 May 2026 04:30:11 |
| Eccentricity: | 0.0005262 |
| inclination: | 35.0009° |
| perigee height: | 493 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 57.1691° |
| argument of perigee: | 309.7163° |
| revolutions per day: | 15.23059580 |
| mean anomaly at epoch: | 50.3087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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