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 28538U 26071.68769441 +.00000000 +00000-0 +12049-3 0 00009
2 28538 63.8246 171.1745 0214843 260.6220 97.0463 13.43369300 04
| Epoch (UTC): | 12 March 2026 16:30:16 |
| Eccentricity: | 0.0214843 |
| inclination: | 63.8246° |
| perigee height: | 936 km |
| apogee height: | 1257 km |
| right ascension of ascending node: | 171.1745° |
| argument of perigee: | 260.6220° |
| revolutions per day: | 13.43369300 |
| mean anomaly at epoch: | 97.0463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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