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 55010U 26075.28374602 +.00000000 +00000-0 +90840-3 0 00000
2 55010 97.3297 141.0757 0006677 98.1946 262.0063 15.49679570 00
| Epoch (UTC): | 16 March 2026 06:48:35 |
| Eccentricity: | 0.0006677 |
| inclination: | 97.3297° |
| perigee height: | 413 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 141.0757° |
| argument of perigee: | 98.1946° |
| revolutions per day: | 15.49679570 |
| mean anomaly at epoch: | 262.0063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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