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 52084U 26145.57815286 +.00000000 +00000-0 +19913-4 0 00009
2 52084 63.3977 259.1916 0049989 353.2331 6.8015 13.45459108 08
| Epoch (UTC): | 25 May 2026 13:52:32 |
| Eccentricity: | 0.0049989 |
| inclination: | 63.3977° |
| perigee height: | 1052 km |
| apogee height: | 1126 km |
| right ascension of ascending node: | 259.1916° |
| argument of perigee: | 353.2331° |
| revolutions per day: | 13.45459108 |
| mean anomaly at epoch: | 6.8015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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