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 27403U 26153.03040764 +.00000000 +00000-0 +00000-0 0 00000
2 27403 7.6772 66.8163 0003641 209.6897 345.7189 0.99023612 01
| Epoch (UTC): | 02 June 2026 00:43:47 |
| Eccentricity: | 0.0003641 |
| inclination: | 7.6772° |
| perigee height: | 36125 km |
| apogee height: | 36156 km |
| right ascension of ascending node: | 66.8163° |
| argument of perigee: | 209.6897° |
| revolutions per day: | 0.99023612 |
| mean anomaly at epoch: | 345.7189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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