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 06324U 26073.06482409 +.00000000 +00000-0 +94733-4 0 00009
2 06324 74.0765 306.1142 0008768 336.6817 23.3942 14.45283001 07
| Epoch (UTC): | 14 March 2026 01:33:20 |
| Eccentricity: | 0.0008768 |
| inclination: | 74.0765° |
| perigee height: | 735 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 306.1142° |
| argument of perigee: | 336.6817° |
| revolutions per day: | 14.45283001 |
| mean anomaly at epoch: | 23.3942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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