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 63873U 26145.45801994 +.00000000 +00000-0 +15978-3 0 00001
2 63873 70.0023 40.8481 0002762 269.3955 90.6887 14.98334880 08
| Epoch (UTC): | 25 May 2026 10:59:32 |
| Eccentricity: | 0.0002762 |
| inclination: | 70.0023° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 40.8481° |
| argument of perigee: | 269.3955° |
| revolutions per day: | 14.98334880 |
| mean anomaly at epoch: | 90.6887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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