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 52300U 26145.23115176 +.00000000 +00000-0 +21437-3 0 00007
2 52300 53.2131 115.5128 0001008 60.0974 300.0118 15.08858260 01
| Epoch (UTC): | 25 May 2026 05:32:51 |
| Eccentricity: | 0.0001008 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 115.5128° |
| argument of perigee: | 60.0974° |
| revolutions per day: | 15.08858260 |
| mean anomaly at epoch: | 300.0118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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