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 26070.76113019 +.00000000 +00000-0 +93863-4 0 00001
2 23827 99.0378 91.6336 0002843 202.8313 157.2738 14.23703449 04
| Epoch (UTC): | 11 March 2026 18:16:01 |
| Eccentricity: | 0.0002843 |
| inclination: | 99.0378° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 91.6336° |
| argument of perigee: | 202.8313° |
| revolutions per day: | 14.23703449 |
| mean anomaly at epoch: | 157.2738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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