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 51988U 26145.46854316 +.00000000 +00000-0 +60372-3 0 00000
2 51988 53.2128 54.4458 0001547 103.4862 256.6303 15.08792332 00
| Epoch (UTC): | 25 May 2026 11:14:42 |
| Eccentricity: | 0.0001547 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 54.4458° |
| argument of perigee: | 103.4862° |
| revolutions per day: | 15.08792332 |
| mean anomaly at epoch: | 256.6303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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