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 54699U 26145.64254676 +.00000000 +00000-0 +57512-4 0 00008
2 54699 59.9975 314.9525 0010018 159.3871 200.7571 14.29519540 04
| Epoch (UTC): | 25 May 2026 15:25:16 |
| Eccentricity: | 0.0010018 |
| inclination: | 59.9975° |
| perigee height: | 786 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 314.9525° |
| argument of perigee: | 159.3871° |
| revolutions per day: | 14.29519540 |
| mean anomaly at epoch: | 200.7571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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