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 27597U 26106.60587751 +.00000000 +00000-0 +81764-4 0 00007
2 27597 98.7831 65.3616 0000335 143.3690 216.7514 14.29313519 06
| Epoch (UTC): | 16 April 2026 14:32:27 |
| Eccentricity: | 0.0000335 |
| inclination: | 98.7831° |
| perigee height: | 794 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 65.3616° |
| argument of perigee: | 143.3690° |
| revolutions per day: | 14.29313519 |
| mean anomaly at epoch: | 216.7514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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