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 04370U 26075.18955108 +.00000000 +00000-0 +10497-3 0 00008
2 04370 74.0368 108.7734 0015838 289.7247 70.2212 14.63296215 01
| Epoch (UTC): | 16 March 2026 04:32:57 |
| Eccentricity: | 0.0015838 |
| inclination: | 74.0368° |
| perigee height: | 671 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 108.7734° |
| argument of perigee: | 289.7247° |
| revolutions per day: | 14.63296215 |
| mean anomaly at epoch: | 70.2212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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