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 42834U 26106.44545285 +.00000000 +00000-0 +20039-3 0 00003
2 42834 97.4157 270.1098 0007248 274.8860 85.1542 15.08470190 09
| Epoch (UTC): | 16 April 2026 10:41:27 |
| Eccentricity: | 0.0007248 |
| inclination: | 97.4157° |
| perigee height: | 536 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 270.1098° |
| argument of perigee: | 274.8860° |
| revolutions per day: | 15.08470190 |
| mean anomaly at epoch: | 85.1542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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