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 00051U 26087.98474037 +.00000000 +00000-0 +28545-3 0 00001
2 00051 47.2135 297.5335 0108114 319.0199 40.2503 12.18377278 01
| Epoch (UTC): | 28 March 2026 23:38:01 |
| Eccentricity: | 0.0108114 |
| inclination: | 47.2135° |
| perigee height: | 1513 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 297.5335° |
| argument of perigee: | 319.0199° |
| revolutions per day: | 12.18377278 |
| mean anomaly at epoch: | 40.2503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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