▸Orbital parameters

Orbit class	LEO
Inclination	88.9999°
Eccentricity	0.0004443
Period	106.5 min
Apogee	1,066 km
Perigee	1,059 km
Mean motion	13.52695970 rev/day
RAAN	266.5595°
Arg of perigee	50.2374°
Mean anomaly	309.9169°
B*	7.0575e-5
Rev at epoch	2,235

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 67556U 26015A 26187.73152536 .00000059 00000-0 70575-4 0 9991

2 67556 88.9999 266.5595 0004443 50.2374 309.9169 13.52695970 22353

▸ source OMM (JSON)

{
  "OBJECT_NAME": "MR-2",
  "OBJECT_ID": "2026-015A",
  "EPOCH": "2026-07-06T17:33:23.791+00:00",
  "MEAN_MOTION": 13.5269597,
  "ECCENTRICITY": 0.0004443,
  "INCLINATION": 88.9999,
  "RA_OF_ASC_NODE": 266.5595,
  "ARG_OF_PERICENTER": 50.2374,
  "MEAN_ANOMALY": 309.9169,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67556,
  "REV_AT_EPOCH": 2235,
  "BSTAR": 0.000070575,
  "MEAN_MOTION_DOT": 5.9e-7,
  "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	MR-2
Operator	Open Cosmos/BarcelonaHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Spain
Launch date	Jan 22, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	20HIGHvia 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/67556

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