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 59102U 26145.32473668 +.00000000 +00000-0 +28840-3 0 00002
2 59102 97.8281 281.9739 0016543 88.4259 271.8862 15.05886710 03
| Epoch (UTC): | 25 May 2026 07:47:37 |
| Eccentricity: | 0.0016543 |
| inclination: | 97.8281° |
| perigee height: | 537 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 281.9739° |
| argument of perigee: | 88.4259° |
| revolutions per day: | 15.05886710 |
| mean anomaly at epoch: | 271.8862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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