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 03093U 26106.85444890 +.00000000 +00000-0 +11451-3 0 00000
2 03093 105.7977 334.2454 0319146 205.4785 165.4155 12.83601471 03
| Epoch (UTC): | 16 April 2026 20:30:24 |
| Eccentricity: | 0.0319146 |
| inclination: | 105.7977° |
| perigee height: | 1081 km |
| apogee height: | 1573 km |
| right ascension of ascending node: | 334.2454° |
| argument of perigee: | 205.4785° |
| revolutions per day: | 12.83601471 |
| mean anomaly at epoch: | 165.4155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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