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 26044.10377956 +.00000000 +00000-0 -69454-3 0 00005
2 00051 47.2132 73.3118 0110165 188.7298 171.1573 12.18378704 03
| Epoch (UTC): | 13 February 2026 02:29:26 |
| Eccentricity: | 0.0110165 |
| inclination: | 47.2132° |
| perigee height: | 1512 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 73.3118° |
| argument of perigee: | 188.7298° |
| revolutions per day: | 12.18378704 |
| mean anomaly at epoch: | 171.1573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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