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 63888U 26145.14525434 +.00000000 +00000-0 +25315-3 0 00001
2 63888 70.0023 41.7581 0002582 269.3127 90.7736 14.98338044 06
| Epoch (UTC): | 25 May 2026 03:29:09 |
| Eccentricity: | 0.0002582 |
| inclination: | 70.0023° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.7581° |
| argument of perigee: | 269.3127° |
| revolutions per day: | 14.98338044 |
| mean anomaly at epoch: | 90.7736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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