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 37389U 26032.51626419 +.00000000 +00000-0 +85268-4 0 00003
2 37389 98.3362 16.1106 0014709 25.6259 334.5648 14.25155551 05
| Epoch (UTC): | 01 February 2026 12:23:25 |
| Eccentricity: | 0.0014709 |
| inclination: | 98.3362° |
| perigee height: | 797 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 16.1106° |
| argument of perigee: | 25.6259° |
| revolutions per day: | 14.25155551 |
| mean anomaly at epoch: | 334.5648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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