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 26073.57227755 +.00000000 +00000-0 +94503-4 0 00008
2 23827 99.0373 94.5216 0002986 193.6514 166.4583 14.23704699 04
| Epoch (UTC): | 14 March 2026 13:44:04 |
| Eccentricity: | 0.0002986 |
| inclination: | 99.0373° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 94.5216° |
| argument of perigee: | 193.6514° |
| revolutions per day: | 14.23704699 |
| mean anomaly at epoch: | 166.4583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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