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 51990U 26145.38574466 +.00000000 +00000-0 +57158-3 0 00007
2 51990 53.2135 34.8171 0001928 97.5303 262.5909 15.08792883 00
| Epoch (UTC): | 25 May 2026 09:15:28 |
| Eccentricity: | 0.0001928 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.8171° |
| argument of perigee: | 97.5303° |
| revolutions per day: | 15.08792883 |
| mean anomaly at epoch: | 262.5909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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