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 26087.32981581 +.00000000 +00000-0 +38166-3 0 00009
2 39151 98.1084 228.8894 0013749 73.4438 286.8289 14.93225120 07
| Epoch (UTC): | 28 March 2026 07:54:56 |
| Eccentricity: | 0.0013749 |
| inclination: | 98.1084° |
| perigee height: | 578 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 228.8894° |
| argument of perigee: | 73.4438° |
| revolutions per day: | 14.93225120 |
| mean anomaly at epoch: | 286.8289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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