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 23908U 26071.18916685 +.00000000 +00000-0 +33517-3 0 00007
2 23908 63.3193 85.3737 0846779 47.9743 319.0275 13.45895756 07
| Epoch (UTC): | 12 March 2026 04:32:24 |
| Eccentricity: | 0.0846779 |
| inclination: | 63.3193° |
| perigee height: | 455 km |
| apogee height: | 1720 km |
| right ascension of ascending node: | 85.3737° |
| argument of perigee: | 47.9743° |
| revolutions per day: | 13.45895756 |
| mean anomaly at epoch: | 319.0275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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