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 26086.86600721 +.00000000 +00000-0 +46949-3 0 00002
2 23908 63.3212 44.3723 0847460 48.2233 318.8122 13.45970231 05
| Epoch (UTC): | 27 March 2026 20:47:03 |
| Eccentricity: | 0.0847460 |
| inclination: | 63.3212° |
| perigee height: | 454 km |
| apogee height: | 1720 km |
| right ascension of ascending node: | 44.3723° |
| argument of perigee: | 48.2233° |
| revolutions per day: | 13.45970231 |
| mean anomaly at epoch: | 318.8122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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