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 61642U 26145.58335647 +.00000000 +00000-0 +16517-2 0 00003
2 61642 42.9947 74.6377 0017726 196.7433 58.8405 15.48584260 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0017726 |
| inclination: | 42.9947° |
| perigee height: | 409 km |
| apogee height: | 433 km |
| right ascension of ascending node: | 74.6377° |
| argument of perigee: | 196.7433° |
| revolutions per day: | 15.48584260 |
| mean anomaly at epoch: | 58.8405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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