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 23179U 26106.66033985 +.00000000 +00000-0 +21019-4 0 00007
2 23179 82.9447 72.7280 0033711 261.7893 271.4217 13.76807350 09
| Epoch (UTC): | 16 April 2026 15:50:53 |
| Eccentricity: | 0.0033711 |
| inclination: | 82.9447° |
| perigee height: | 950 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 72.7280° |
| argument of perigee: | 261.7893° |
| revolutions per day: | 13.76807350 |
| mean anomaly at epoch: | 271.4217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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