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 15172U 26088.23837007 +.00000000 +00000-0 -93012-4 0 00003
2 15172 82.6024 197.9981 0006460 191.7023 180.8331 12.42604456 01
| Epoch (UTC): | 29 March 2026 05:43:15 |
| Eccentricity: | 0.0006460 |
| inclination: | 82.6024° |
| perigee height: | 1490 km |
| apogee height: | 1501 km |
| right ascension of ascending node: | 197.9981° |
| argument of perigee: | 191.7023° |
| revolutions per day: | 12.42604456 |
| mean anomaly at epoch: | 180.8331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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