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 42695U 26152.16483435 +.00000000 +00000-0 +00000-0 0 00009
2 42695 0.0283 272.9283 0002488 152.7981 340.5525 1.00275742 01
| Epoch (UTC): | 01 June 2026 03:57:21 |
| Eccentricity: | 0.0002488 |
| inclination: | 0.0283° |
| perigee height: | 35775 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 272.9283° |
| argument of perigee: | 152.7981° |
| revolutions per day: | 1.00275742 |
| mean anomaly at epoch: | 340.5525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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