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 27431U 26106.84728919 +.00000000 +00000-0 +71288-4 0 00003
2 27431 98.9583 157.4403 0016239 58.0681 302.2066 14.10216286 04
| Epoch (UTC): | 16 April 2026 20:20:05 |
| Eccentricity: | 0.0016239 |
| inclination: | 98.9583° |
| perigee height: | 847 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 157.4403° |
| argument of perigee: | 58.0681° |
| revolutions per day: | 14.10216286 |
| mean anomaly at epoch: | 302.2066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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