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 04256U 26088.16905988 +.00000000 +00000-0 +11577-3 0 00004
2 04256 70.0082 136.9134 0019374 178.5546 181.5621 13.99174268 07
| Epoch (UTC): | 29 March 2026 04:03:26 |
| Eccentricity: | 0.0019374 |
| inclination: | 70.0082° |
| perigee height: | 883 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 136.9134° |
| argument of perigee: | 178.5546° |
| revolutions per day: | 13.99174268 |
| mean anomaly at epoch: | 181.5621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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