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 52295U 26145.33051976 +.00000000 +00000-0 -27339-3 0 00006
2 52295 53.2138 115.0639 0001551 73.7438 286.3725 15.08862501 05
| Epoch (UTC): | 25 May 2026 07:55:56 |
| Eccentricity: | 0.0001551 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.0639° |
| argument of perigee: | 73.7438° |
| revolutions per day: | 15.08862501 |
| mean anomaly at epoch: | 286.3725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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