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 60278U 26145.05577272 +.00000000 +00000-0 -13048-4 0 00000
2 60278 53.1591 57.6267 0000862 109.9988 250.1105 15.30197781 08
| Epoch (UTC): | 25 May 2026 01:20:18 |
| Eccentricity: | 0.0000862 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.6267° |
| argument of perigee: | 109.9988° |
| revolutions per day: | 15.30197781 |
| mean anomaly at epoch: | 250.1105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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