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 52297U 26145.32684924 +.00000000 +00000-0 +35807-3 0 00000
2 52297 53.2135 115.0824 0001413 77.1409 282.9741 15.08818423 07
| Epoch (UTC): | 25 May 2026 07:50:39 |
| Eccentricity: | 0.0001413 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.0824° |
| argument of perigee: | 77.1409° |
| revolutions per day: | 15.08818423 |
| mean anomaly at epoch: | 282.9741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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