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 26106.78932422 +.00000000 +00000-0 +47936-4 0 00003
2 25693 64.5539 250.6143 0032728 229.8453 129.9787 14.84202935 06
| Epoch (UTC): | 16 April 2026 18:56:37 |
| Eccentricity: | 0.0032728 |
| inclination: | 64.5539° |
| perigee height: | 593 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 250.6143° |
| argument of perigee: | 229.8453° |
| revolutions per day: | 14.84202935 |
| mean anomaly at epoch: | 129.9787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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