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 115U 60002D 25167.20209976 .00002811 00000-0 27365-3 0 9999
2 115 48.1628 97.2502 0027215 51.1923 309.1419 14.95119351484474
| Epoch (UTC): | 16 June 2025 04:51:01 |
| Eccentricity: | 0.0027215 |
| inclination: | 48.1628° |
| perigee height: | 563 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 97.2502° |
| argument of perigee: | 51.1923° |
| revolutions per day: | 14.95119351 |
| mean anomaly at epoch: | 309.1419° |
| orbit number at epoch: | 48447 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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