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 data is extracted from the following two-line orbital elements,
1 48274U 21035A 23157.60162035 .00020860 00000-0 25608-3 0 9997
2 48274 41.4734 220.2070 0003424 306.1503 53.9018 15.59800394120186
| Epoch (UTC): | 06 June 2023 14:26:19 |
| Eccentricity: | 0.0003424 |
| inclination: | 41.4734° |
| perigee height: | 386 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 220.2070° |
| argument of perigee: | 306.1503° |
| revolutions per day: | 15.59800394 |
| mean anomaly at epoch: | 53.9018° |
| orbit number at epoch: | 12018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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