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 60510U 26145.50910534 +.00000000 +00000-0 +37282-3 0 00005
2 60510 97.3731 229.0607 0003802 34.9532 325.1963 15.39494688 05
| Epoch (UTC): | 25 May 2026 12:13:06 |
| Eccentricity: | 0.0003802 |
| inclination: | 97.3731° |
| perigee height: | 445 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 229.0607° |
| argument of perigee: | 34.9532° |
| revolutions per day: | 15.39494688 |
| mean anomaly at epoch: | 325.1963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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