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 52992U 26145.24454667 +.00000000 +00000-0 +40439-4 0 00000
2 52992 53.2134 120.4620 0001152 78.4229 281.6892 15.08838695 02
| Epoch (UTC): | 25 May 2026 05:52:08 |
| Eccentricity: | 0.0001152 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 120.4620° |
| argument of perigee: | 78.4229° |
| revolutions per day: | 15.08838695 |
| mean anomaly at epoch: | 281.6892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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