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 26040.72518992 +.00000000 +00000-0 +17290-3 0 00002
2 23908 63.3205 165.0290 0845053 47.4895 319.4433 13.45810197 04
| Epoch (UTC): | 09 February 2026 17:24:16 |
| Eccentricity: | 0.0845053 |
| inclination: | 63.3205° |
| perigee height: | 457 km |
| apogee height: | 1719 km |
| right ascension of ascending node: | 165.0290° |
| argument of perigee: | 47.4895° |
| revolutions per day: | 13.45810197 |
| mean anomaly at epoch: | 319.4433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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