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 26041.61684196 +.00000000 +00000-0 +16781-3 0 00005
2 23908 63.3205 162.6976 0845078 47.5056 319.4293 13.45812126 03
| Epoch (UTC): | 10 February 2026 14:48:15 |
| Eccentricity: | 0.0845078 |
| inclination: | 63.3205° |
| perigee height: | 457 km |
| apogee height: | 1719 km |
| right ascension of ascending node: | 162.6976° |
| argument of perigee: | 47.5056° |
| revolutions per day: | 13.45812126 |
| mean anomaly at epoch: | 319.4293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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