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 21015U 26037.61673667 +.00000000 +00000-0 +11849-3 0 00008
2 21015 74.0493 105.1271 0022651 306.4031 53.5033 14.37255783 02
| Epoch (UTC): | 06 February 2026 14:48:06 |
| Eccentricity: | 0.0022651 |
| inclination: | 74.0493° |
| perigee height: | 751 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 105.1271° |
| argument of perigee: | 306.4031° |
| revolutions per day: | 14.37255783 |
| mean anomaly at epoch: | 53.5033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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