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 57206U 26145.62726534 +.00000000 +00000-0 +90326-3 0 00009
2 57206 97.5055 224.1214 0004859 131.9174 228.2497 15.59661769 00
| Epoch (UTC): | 25 May 2026 15:03:15 |
| Eccentricity: | 0.0004859 |
| inclination: | 97.5055° |
| perigee height: | 385 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 224.1214° |
| argument of perigee: | 131.9174° |
| revolutions per day: | 15.59661769 |
| mean anomaly at epoch: | 228.2497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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