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 27453U 26100.17587568 +.00000000 +00000-0 +11332-3 0 00003
2 27453 98.8594 65.1500 0011467 183.4995 176.6106 14.26208327 03
| Epoch (UTC): | 10 April 2026 04:13:15 |
| Eccentricity: | 0.0011467 |
| inclination: | 98.8594° |
| perigee height: | 796 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 65.1500° |
| argument of perigee: | 183.4995° |
| revolutions per day: | 14.26208327 |
| mean anomaly at epoch: | 176.6106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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