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 60265U 26145.16751286 +.00000000 +00000-0 +38642-4 0 00003
2 60265 53.1621 57.4892 0001286 79.1277 280.9868 15.29364617 09
| Epoch (UTC): | 25 May 2026 04:01:13 |
| Eccentricity: | 0.0001286 |
| inclination: | 53.1621° |
| perigee height: | 477 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 57.4892° |
| argument of perigee: | 79.1277° |
| revolutions per day: | 15.29364617 |
| mean anomaly at epoch: | 280.9868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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