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 26033.51761801 +.00000000 +00000-0 +14875-3 0 00006
2 23908 63.3195 183.8717 0844610 47.3812 319.5358 13.45792935 06
| Epoch (UTC): | 02 February 2026 12:25:22 |
| Eccentricity: | 0.0844610 |
| inclination: | 63.3195° |
| perigee height: | 457 km |
| apogee height: | 1718 km |
| right ascension of ascending node: | 183.8717° |
| argument of perigee: | 47.3812° |
| revolutions per day: | 13.45792935 |
| mean anomaly at epoch: | 319.5358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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