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 15370U 26042.08502838 +.00000000 +00000-0 +52362-4 0 00009
2 15370 82.5145 281.5118 0021456 62.9236 297.4167 14.86034079 03
| Epoch (UTC): | 11 February 2026 02:02:26 |
| Eccentricity: | 0.0021456 |
| inclination: | 82.5145° |
| perigee height: | 595 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 281.5118° |
| argument of perigee: | 62.9236° |
| revolutions per day: | 14.86034079 |
| mean anomaly at epoch: | 297.4167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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