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 51873U 26145.66345763 +.00000000 +00000-0 +10418-2 0 00001
2 51873 53.2162 14.0139 0004960 103.6294 256.5257 15.21037948 09
| Epoch (UTC): | 25 May 2026 15:55:22 |
| Eccentricity: | 0.0004960 |
| inclination: | 53.2162° |
| perigee height: | 499 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 14.0139° |
| argument of perigee: | 103.6294° |
| revolutions per day: | 15.21037948 |
| mean anomaly at epoch: | 256.5257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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