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 48640U 26145.61929050 +.00000000 +00000-0 +24535-4 0 00008
2 48640 53.1584 116.0104 0001444 106.3526 253.7634 15.31707170 01
| Epoch (UTC): | 25 May 2026 14:51:46 |
| Eccentricity: | 0.0001444 |
| inclination: | 53.1584° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 116.0104° |
| argument of perigee: | 106.3526° |
| revolutions per day: | 15.31707170 |
| mean anomaly at epoch: | 253.7634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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