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 27842U 26150.53116807 +.00000000 +00000-0 +14262-3 0 00009
2 27842 98.6850 159.2043 0008618 207.0457 153.0273 14.23918915 07
| Epoch (UTC): | 30 May 2026 12:44:52 |
| Eccentricity: | 0.0008618 |
| inclination: | 98.6850° |
| perigee height: | 806 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 159.2043° |
| argument of perigee: | 207.0457° |
| revolutions per day: | 14.23918915 |
| mean anomaly at epoch: | 153.0273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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