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 40030U 26071.23768737 +.00000000 +00000-0 +53184-3 0 00003
2 40030 98.0852 62.9275 0007375 191.8808 168.2249 15.13589176 07
| Epoch (UTC): | 12 March 2026 05:42:16 |
| Eccentricity: | 0.0007375 |
| inclination: | 98.0852° |
| perigee height: | 520 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 62.9275° |
| argument of perigee: | 191.8808° |
| revolutions per day: | 15.13589176 |
| mean anomaly at epoch: | 168.2249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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