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 07530U 26103.77267182 +.00000000 +00000-0 +12067-3 0 00009
2 07530 101.9944 116.3401 0011879 253.5120 287.5368 12.53697056 08
| Epoch (UTC): | 13 April 2026 18:32:38 |
| Eccentricity: | 0.0011879 |
| inclination: | 101.9944° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 116.3401° |
| argument of perigee: | 253.5120° |
| revolutions per day: | 12.53697056 |
| mean anomaly at epoch: | 287.5368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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