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 01520U 26145.40799046 +.00000000 +00000-0 +21777-3 0 00005
2 01520 89.8967 122.7135 0070131 166.0680 358.3002 13.36273583 09
| Epoch (UTC): | 25 May 2026 09:47:30 |
| Eccentricity: | 0.0070131 |
| inclination: | 89.8967° |
| perigee height: | 1071 km |
| apogee height: | 1176 km |
| right ascension of ascending node: | 122.7135° |
| argument of perigee: | 166.0680° |
| revolutions per day: | 13.36273583 |
| mean anomaly at epoch: | 358.3002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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