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 26114.27713935 +.00000000 +00000-0 +94198-4 0 00000
2 27453 98.8612 79.4124 0012223 143.4922 216.7093 14.26213292 09
| Epoch (UTC): | 24 April 2026 06:39:04 |
| Eccentricity: | 0.0012223 |
| inclination: | 98.8612° |
| perigee height: | 796 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 79.4124° |
| argument of perigee: | 143.4922° |
| revolutions per day: | 14.26213292 |
| mean anomaly at epoch: | 216.7093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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