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 42942U 26145.60797279 +.00000000 +00000-0 +00000-0 0 00009
2 42942 0.0103 329.2793 0002573 86.9321 167.9582 1.00270835 02
| Epoch (UTC): | 25 May 2026 14:35:28 |
| Eccentricity: | 0.0002573 |
| inclination: | 0.0103° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 329.2793° |
| argument of perigee: | 86.9321° |
| revolutions per day: | 1.00270835 |
| mean anomaly at epoch: | 167.9582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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