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 18959U 26161.49885666 +.00000000 +00000-0 +35718-4 0 00001
2 18959 82.5370 82.5930 0017571 106.8565 253.4580 14.85742964 05
| Epoch (UTC): | 10 June 2026 11:58:21 |
| Eccentricity: | 0.0017571 |
| inclination: | 82.5370° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 82.5930° |
| argument of perigee: | 106.8565° |
| revolutions per day: | 14.85742964 |
| mean anomaly at epoch: | 253.4580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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