▸Orbital parameters

Orbit class	SSO
Inclination	97.4554°
Eccentricity	0.0000637
Period	94.8 min
Apogee	507 km
Perigee	506 km
Mean motion	15.19707004 rev/day
RAAN	146.4910°
Arg of perigee	100.8164°
Mean anomaly	259.3143°
B*	2.7707e-4
Rev at epoch	1,498

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 68427U 26067M 26188.19102505 .00005850 00000-0 27707-3 0 9990

2 68427 97.4554 146.4910 0000637 100.8164 259.3143 15.19707004 14987

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EMISAR",
  "OBJECT_ID": "2026-067M",
  "EPOCH": "2026-07-07T04:35:04.564+00:00",
  "MEAN_MOTION": 15.19707004,
  "ECCENTRICITY": 0.0000637,
  "INCLINATION": 97.4554,
  "RA_OF_ASC_NODE": 146.491,
  "ARG_OF_PERICENTER": 100.8164,
  "MEAN_ANOMALY": 259.3143,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68427,
  "REV_AT_EPOCH": 1498,
  "BSTAR": 0.00027707,
  "MEAN_MOTION_DOT": 0.0000585,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	EMISAR
Operator	Romanian InSpace EngineeringHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Romania
Launch date	Mar 30, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/68427

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.