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 15495U 26129.45547845 +.00000000 +00000-0 +31472-4 0 00000
2 15495 82.5256 21.7205 0020377 46.6857 313.6054 14.86171863 03
| Epoch (UTC): | 09 May 2026 10:55:53 |
| Eccentricity: | 0.0020377 |
| inclination: | 82.5256° |
| perigee height: | 596 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 21.7205° |
| argument of perigee: | 46.6857° |
| revolutions per day: | 14.86171863 |
| mean anomaly at epoch: | 313.6054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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