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 42921U 26145.51111000 +.00000000 +00000-0 +12606-3 0 00006
2 42921 0.0497 315.5872 0010481 83.6663 320.8225 15.00806116 07
| Epoch (UTC): | 25 May 2026 12:15:59 |
| Eccentricity: | 0.0010481 |
| inclination: | 0.0497° |
| perigee height: | 557 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 315.5872° |
| argument of perigee: | 83.6663° |
| revolutions per day: | 15.00806116 |
| mean anomaly at epoch: | 320.8225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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