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 21263U 26072.96129373 +.00000000 +00000-0 +77619-4 0 00008
2 21263 98.6158 62.8960 0012747 310.0056 50.0005 14.26719246 02
| Epoch (UTC): | 13 March 2026 23:04:15 |
| Eccentricity: | 0.0012747 |
| inclination: | 98.6158° |
| perigee height: | 794 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 62.8960° |
| argument of perigee: | 310.0056° |
| revolutions per day: | 14.26719246 |
| mean anomaly at epoch: | 50.0005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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