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 60466U 26145.62140220 +.00000000 +00000-0 +40348-3 0 00002
2 60466 34.9914 278.4866 0007399 52.6404 307.4987 15.35731030 00
| Epoch (UTC): | 25 May 2026 14:54:49 |
| Eccentricity: | 0.0007399 |
| inclination: | 34.9914° |
| perigee height: | 454 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 278.4866° |
| argument of perigee: | 52.6404° |
| revolutions per day: | 15.35731030 |
| mean anomaly at epoch: | 307.4987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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