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 26039.61062257 +.00000000 +00000-0 +17992-3 0 00005
2 23908 63.3204 167.9429 0844980 47.4730 319.4574 13.45807848 09
| Epoch (UTC): | 08 February 2026 14:39:17 |
| Eccentricity: | 0.0844980 |
| inclination: | 63.3204° |
| perigee height: | 457 km |
| apogee height: | 1719 km |
| right ascension of ascending node: | 167.9429° |
| argument of perigee: | 47.4730° |
| revolutions per day: | 13.45807848 |
| mean anomaly at epoch: | 319.4574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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