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 01328U 26154.16634816 +.00000000 +00000-0 +15106-3 0 00006
2 01328 41.1843 77.2684 0242005 233.1526 124.6812 13.38928290 05
| Epoch (UTC): | 03 June 2026 03:59:32 |
| Eccentricity: | 0.0242005 |
| inclination: | 41.1843° |
| perigee height: | 932 km |
| apogee height: | 1295 km |
| right ascension of ascending node: | 77.2684° |
| argument of perigee: | 233.1526° |
| revolutions per day: | 13.38928290 |
| mean anomaly at epoch: | 124.6812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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