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 27437U 26159.45695742 +.00000000 +00000-0 +46956-4 0 00005
2 27437 82.9488 156.4922 0042915 208.0525 151.8320 13.76952551 00
| Epoch (UTC): | 08 June 2026 10:58:01 |
| Eccentricity: | 0.0042915 |
| inclination: | 82.9488° |
| perigee height: | 943 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 156.4922° |
| argument of perigee: | 208.0525° |
| revolutions per day: | 13.76952551 |
| mean anomaly at epoch: | 151.8320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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