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 30688U 26088.18675024 +.00000000 +00000-0 +17853-2 0 00001
2 30688 98.6899 167.0154 0014205 10.7279 43.5307 14.33730116 09
| Epoch (UTC): | 29 March 2026 04:28:55 |
| Eccentricity: | 0.0014205 |
| inclination: | 98.6899° |
| perigee height: | 769 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 167.0154° |
| argument of perigee: | 10.7279° |
| revolutions per day: | 14.33730116 |
| mean anomaly at epoch: | 43.5307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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