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 00733U 26069.01057468 +.00000000 +00000-0 +11427-3 0 00008
2 00733 99.1226 82.3655 0031972 257.1553 102.6057 14.34020282 00
| Epoch (UTC): | 10 March 2026 00:15:13 |
| Eccentricity: | 0.0031972 |
| inclination: | 99.1226° |
| perigee height: | 755 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 82.3655° |
| argument of perigee: | 257.1553° |
| revolutions per day: | 14.34020282 |
| mean anomaly at epoch: | 102.6057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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