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 26131.26523552 +.00000000 +00000-0 +75333-4 0 00006
2 07530 101.9918 144.1250 0012127 199.8952 171.1595 12.53697437 05
| Epoch (UTC): | 11 May 2026 06:21:56 |
| Eccentricity: | 0.0012127 |
| inclination: | 101.9918° |
| perigee height: | 1440 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 144.1250° |
| argument of perigee: | 199.8952° |
| revolutions per day: | 12.53697437 |
| mean anomaly at epoch: | 171.1595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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