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 52907U 26145.53261255 +.00000000 +00000-0 +29887-3 0 00000
2 52907 34.9913 281.2385 0010986 233.5495 126.4207 15.23834447 01
| Epoch (UTC): | 25 May 2026 12:46:57 |
| Eccentricity: | 0.0010986 |
| inclination: | 34.9913° |
| perigee height: | 487 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 281.2385° |
| argument of perigee: | 233.5495° |
| revolutions per day: | 15.23834447 |
| mean anomaly at epoch: | 126.4207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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