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 37387U 26114.17588546 +.00000000 +00000-0 +60398-4 0 00009
2 37387 98.7670 181.9831 0012193 57.5678 302.6677 14.21598658 02
| Epoch (UTC): | 24 April 2026 04:13:16 |
| Eccentricity: | 0.0012193 |
| inclination: | 98.7670° |
| perigee height: | 811 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 181.9831° |
| argument of perigee: | 57.5678° |
| revolutions per day: | 14.21598658 |
| mean anomaly at epoch: | 302.6677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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