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 01512U 26145.46782718 +.00000000 +00000-0 +17653-4 0 00009
2 01512 90.0003 212.5905 0068074 313.5785 57.4917 13.33592669 04
| Epoch (UTC): | 25 May 2026 11:13:40 |
| Eccentricity: | 0.0068074 |
| inclination: | 90.0003° |
| perigee height: | 1082 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 212.5905° |
| argument of perigee: | 313.5785° |
| revolutions per day: | 13.33592669 |
| mean anomaly at epoch: | 57.4917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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