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 26159.48382257 +.00000000 +00000-0 +41141-4 0 00004
2 15495 82.5231 353.4811 0017959 306.8319 53.1250 14.86190913 01
| Epoch (UTC): | 08 June 2026 11:36:42 |
| Eccentricity: | 0.0017959 |
| inclination: | 82.5231° |
| perigee height: | 597 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 353.4811° |
| argument of perigee: | 306.8319° |
| revolutions per day: | 14.86190913 |
| mean anomaly at epoch: | 53.1250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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