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 40300U 14070C 25012.69875439 .14599716 24063-5 11754-3 0 9993
2 40300 97.0264 61.4205 0009153 258.8077 101.2201 16.52307711567468
| Epoch (UTC): | 12 January 2025 16:46:12 |
| Eccentricity: | 0.0009153 |
| inclination: | 97.0264° |
| perigee height: | 127 km |
| apogee height: | 139 km |
| right ascension of ascending node: | 61.4205° |
| argument of perigee: | 258.8077° |
| revolutions per day: | 16.52307711 |
| mean anomaly at epoch: | 101.2201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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