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 00115U 60002D 25171.14496511 .00002620 00000-0 25650-3 0 9993
2 00115 48.1636 77.9429 0027298 69.8458 290.5392 14.95142073463901
| Epoch (UTC): | 20 June 2025 03:28:44 |
| Eccentricity: | 0.0027298 |
| inclination: | 48.1636° |
| perigee height: | 563 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 77.9429° |
| argument of perigee: | 69.8458° |
| revolutions per day: | 14.95142073 |
| mean anomaly at epoch: | 290.5392° |
| orbit number at epoch: | 46390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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