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 57389U 26145.46432641 +.00000000 +00000-0 +37752-3 0 00000
2 57389 99.5066 160.7239 0005518 172.2739 187.8571 15.12058512 04
| Epoch (UTC): | 25 May 2026 11:08:37 |
| Eccentricity: | 0.0005518 |
| inclination: | 99.5066° |
| perigee height: | 526 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 160.7239° |
| argument of perigee: | 172.2739° |
| revolutions per day: | 15.12058512 |
| mean anomaly at epoch: | 187.8571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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