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 28654U 26071.65592051 +.00000000 +00000-0 +65925-4 0 00008
2 28654 98.8152 152.7215 0015234 67.7574 292.5213 14.13711671 00
| Epoch (UTC): | 12 March 2026 15:44:31 |
| Eccentricity: | 0.0015234 |
| inclination: | 98.8152° |
| perigee height: | 836 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 152.7215° |
| argument of perigee: | 67.7574° |
| revolutions per day: | 14.13711671 |
| mean anomaly at epoch: | 292.5213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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