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 37154U 26106.72805396 +.00000000 +00000-0 +15145-3 0 00007
2 37154 82.4557 100.7250 0015972 82.6368 89.8959 12.43745600 05
| Epoch (UTC): | 16 April 2026 17:28:23 |
| Eccentricity: | 0.0015972 |
| inclination: | 82.4557° |
| perigee height: | 1478 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 100.7250° |
| argument of perigee: | 82.6368° |
| revolutions per day: | 12.43745600 |
| mean anomaly at epoch: | 89.8959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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