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 26088.11086020 +.00000000 +00000-0 +15677-3 0 00008
2 04370 74.0367 83.9883 0015990 263.8036 96.1310 14.63312676 03
| Epoch (UTC): | 29 March 2026 02:39:38 |
| Eccentricity: | 0.0015990 |
| inclination: | 74.0367° |
| perigee height: | 671 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 83.9883° |
| argument of perigee: | 263.8036° |
| revolutions per day: | 14.63312676 |
| mean anomaly at epoch: | 96.1310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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