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 26049.43504731 +.00000000 +00000-0 -59714-3 0 00007
2 00051 47.2139 56.8145 0109971 204.6236 154.9276 12.18378277 03
| Epoch (UTC): | 18 February 2026 10:26:28 |
| Eccentricity: | 0.0109971 |
| inclination: | 47.2139° |
| perigee height: | 1512 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 56.8145° |
| argument of perigee: | 204.6236° |
| revolutions per day: | 12.18378277 |
| mean anomaly at epoch: | 154.9276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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