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 23827U 26038.01110270 +.00000000 +00000-0 +10347-3 0 00004
2 23827 99.0399 57.9865 0002711 327.8129 32.2883 14.23690337 00
| Epoch (UTC): | 07 February 2026 00:15:59 |
| Eccentricity: | 0.0002711 |
| inclination: | 99.0399° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 57.9865° |
| argument of perigee: | 327.8129° |
| revolutions per day: | 14.23690337 |
| mean anomaly at epoch: | 32.2883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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