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 60027U 26145.09528159 +.00000000 +00000-0 +22347-4 0 00007
2 60027 53.1603 80.5734 0001298 82.4529 277.6619 15.30194347 07
| Epoch (UTC): | 25 May 2026 02:17:12 |
| Eccentricity: | 0.0001298 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.5734° |
| argument of perigee: | 82.4529° |
| revolutions per day: | 15.30194347 |
| mean anomaly at epoch: | 277.6619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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