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 02520U 26087.23051932 +.00000000 +00000-0 -67084-3 0 00009
2 02520 89.8490 31.9111 0015163 31.2020 328.9729 8.58894171 00
| Epoch (UTC): | 28 March 2026 05:31:56 |
| Eccentricity: | 0.0015163 |
| inclination: | 89.8490° |
| perigee height: | 3678 km |
| apogee height: | 3709 km |
| right ascension of ascending node: | 31.9111° |
| argument of perigee: | 31.2020° |
| revolutions per day: | 8.58894171 |
| mean anomaly at epoch: | 328.9729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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