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 23545U 95017A 25139.19677517 .00005354 00000-0 56611-3 0 9993
2 23545 69.9617 146.4071 0004484 312.9977 47.0801 14.89753043608547
| Epoch (UTC): | 19 May 2025 04:43:21 |
| Eccentricity: | 0.0004484 |
| inclination: | 69.9617° |
| perigee height: | 595 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 146.4071° |
| argument of perigee: | 312.9977° |
| revolutions per day: | 14.89753043 |
| mean anomaly at epoch: | 47.0801° |
| orbit number at epoch: | 60854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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