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 25693U 26155.09992098 +.00000000 +00000-0 +80905-4 0 00009
2 25693 64.5540 100.8945 0028456 224.9335 134.9469 14.84249053 07
| Epoch (UTC): | 04 June 2026 02:23:53 |
| Eccentricity: | 0.0028456 |
| inclination: | 64.5540° |
| perigee height: | 596 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 100.8945° |
| argument of perigee: | 224.9335° |
| revolutions per day: | 14.84249053 |
| mean anomaly at epoch: | 134.9469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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