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 51993U 26145.46485360 +.00000000 +00000-0 +15345-3 0 00005
2 51993 53.2117 54.4636 0001266 83.5061 276.6076 15.08827285 04
| Epoch (UTC): | 25 May 2026 11:09:23 |
| Eccentricity: | 0.0001266 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 54.4636° |
| argument of perigee: | 83.5061° |
| revolutions per day: | 15.08827285 |
| mean anomaly at epoch: | 276.6076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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