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 28523U 26106.67568917 +.00000000 +00000-0 +51201-4 0 00000
2 28523 82.9458 92.1113 0038245 151.8449 208.4793 13.88065075 05
| Epoch (UTC): | 16 April 2026 16:12:59 |
| Eccentricity: | 0.0038245 |
| inclination: | 82.9458° |
| perigee height: | 907 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 92.1113° |
| argument of perigee: | 151.8449° |
| revolutions per day: | 13.88065075 |
| mean anomaly at epoch: | 208.4793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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