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 27421U 26140.10864100 +.00000000 +00000-0 +66188-4 0 00005
2 27421 97.9869 180.2128 0129668 4.4476 355.7842 14.54729050 06
| Epoch (UTC): | 20 May 2026 02:36:26 |
| Eccentricity: | 0.0129668 |
| inclination: | 97.9869° |
| perigee height: | 618 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 180.2128° |
| argument of perigee: | 4.4476° |
| revolutions per day: | 14.54729050 |
| mean anomaly at epoch: | 355.7842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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