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 68421U 26145.38399419 +.00000000 +00000-0 +18295-3 0 00006
2 68421 97.4503 104.2025 0001668 58.0826 302.0571 15.18625369 09
| Epoch (UTC): | 25 May 2026 09:12:57 |
| Eccentricity: | 0.0001668 |
| inclination: | 97.4503° |
| perigee height: | 509 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 104.2025° |
| argument of perigee: | 58.0826° |
| revolutions per day: | 15.18625369 |
| mean anomaly at epoch: | 302.0571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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