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 23839U 26145.16354883 +.00000000 +00000-0 +00000-0 0 00004
2 23839 10.5546 46.8450 0003533 16.5517 167.1986 0.99984353 02
| Epoch (UTC): | 25 May 2026 03:55:30 |
| Eccentricity: | 0.0003533 |
| inclination: | 10.5546° |
| perigee height: | 35852 km |
| apogee height: | 35882 km |
| right ascension of ascending node: | 46.8450° |
| argument of perigee: | 16.5517° |
| revolutions per day: | 0.99984353 |
| mean anomaly at epoch: | 167.1986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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