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 40042U 26156.04237671 +.00000000 +00000-0 +69172-3 0 00001
2 40042 98.0948 181.1587 0007713 177.6399 182.4878 15.32815214 01
| Epoch (UTC): | 05 June 2026 01:01:01 |
| Eccentricity: | 0.0007713 |
| inclination: | 98.0948° |
| perigee height: | 462 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 181.1587° |
| argument of perigee: | 177.6399° |
| revolutions per day: | 15.32815214 |
| mean anomaly at epoch: | 182.4878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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