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 26047.05648035 +.00000000 +00000-0 -75717-3 0 00000
2 00051 47.2135 64.1748 0110069 197.5349 162.1624 12.18378428 01
| Epoch (UTC): | 16 February 2026 01:21:19 |
| Eccentricity: | 0.0110069 |
| inclination: | 47.2135° |
| perigee height: | 1512 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 64.1748° |
| argument of perigee: | 197.5349° |
| revolutions per day: | 12.18378428 |
| mean anomaly at epoch: | 162.1624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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