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 61228U 24173B 25308.14047046 .18698425 25528-5 32238-3 0 9991
2 61228 97.3240 34.9924 0009730 265.1758 94.8434 16.47398128 62784
| Epoch (UTC): | 04 November 2025 03:22:16 |
| Eccentricity: | 0.0009730 |
| inclination: | 97.3240° |
| perigee height: | 140 km |
| apogee height: | 152 km |
| right ascension of ascending node: | 34.9924° |
| argument of perigee: | 265.1758° |
| revolutions per day: | 16.47398128 |
| mean anomaly at epoch: | 94.8434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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