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 61895U 26145.62171766 +.00000000 +00000-0 +41100-3 0 00005
2 61895 97.4139 223.3190 0011696 114.3947 245.8516 15.29867464 09
| Epoch (UTC): | 25 May 2026 14:55:16 |
| Eccentricity: | 0.0011696 |
| inclination: | 97.4139° |
| perigee height: | 468 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 223.3190° |
| argument of perigee: | 114.3947° |
| revolutions per day: | 15.29867464 |
| mean anomaly at epoch: | 245.8516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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