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 52644U 26145.37468782 +.00000000 +00000-0 -20351-4 0 00003
2 52644 53.2145 274.8652 0001140 101.0290 259.0830 15.08837183 07
| Epoch (UTC): | 25 May 2026 08:59:33 |
| Eccentricity: | 0.0001140 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 274.8652° |
| argument of perigee: | 101.0290° |
| revolutions per day: | 15.08837183 |
| mean anomaly at epoch: | 259.0830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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