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 39151U 26106.35966903 +.00000000 +00000-0 +14918-3 0 00004
2 39151 98.1128 248.5125 0012765 13.6936 346.4627 14.93356649 08
| Epoch (UTC): | 16 April 2026 08:37:55 |
| Eccentricity: | 0.0012765 |
| inclination: | 98.1128° |
| perigee height: | 579 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 248.5125° |
| argument of perigee: | 13.6936° |
| revolutions per day: | 14.93356649 |
| mean anomaly at epoch: | 346.4627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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