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 51628U 26145.42944256 +.00000000 +00000-0 -18801-2 0 00000
2 51628 87.8852 40.7972 0002130 83.6028 276.5342 13.10374194 06
| Epoch (UTC): | 25 May 2026 10:18:23 |
| Eccentricity: | 0.0002130 |
| inclination: | 87.8852° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7972° |
| argument of perigee: | 83.6028° |
| revolutions per day: | 13.10374194 |
| mean anomaly at epoch: | 276.5342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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