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 26064.18241322 +.00000000 +00000-0 +14020-3 0 00008
2 04370 74.0384 129.8851 0015557 311.9874 47.9967 14.63282037 00
| Epoch (UTC): | 05 March 2026 04:22:40 |
| Eccentricity: | 0.0015557 |
| inclination: | 74.0384° |
| perigee height: | 672 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 129.8851° |
| argument of perigee: | 311.9874° |
| revolutions per day: | 14.63282037 |
| mean anomaly at epoch: | 47.9967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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